Question

A simple formula to estimate the upward velocity of a rocket (neglecting the aerodynamic drag) is:

Answer 1

Answer:

Test code:

>>u=10;

>>g=9.8;

>>q=100;

>>m0=100;

>>vstar=10;

>>tstar=fzero_rocket_example(u, g, q, m0, vstar)

Explanation:

See attached image